IT8821640A0 - AIRCRAFT PYLON. - Google Patents

AIRCRAFT PYLON.

Info

Publication number
IT8821640A0
IT8821640A0 IT8821640A IT2164088A IT8821640A0 IT 8821640 A0 IT8821640 A0 IT 8821640A0 IT 8821640 A IT8821640 A IT 8821640A IT 2164088 A IT2164088 A IT 2164088A IT 8821640 A0 IT8821640 A0 IT 8821640A0
Authority
IT
Italy
Prior art keywords
aircraft pylon
pylon
aircraft
Prior art date
Application number
IT8821640A
Other languages
Italian (it)
Other versions
IT1226367B (en
Inventor
Bruce Joseph Gordon
Original Assignee
Gen Electric
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Gen Electric filed Critical Gen Electric
Publication of IT8821640A0 publication Critical patent/IT8821640A0/en
Application granted granted Critical
Publication of IT1226367B publication Critical patent/IT1226367B/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/04—Power-plant nacelles, fairings, or cowlings associated with fuselages
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
IT8821640A 1987-08-05 1988-08-04 PLANE PILON. IT1226367B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/081,772 US4966338A (en) 1987-08-05 1987-08-05 Aircraft pylon

Publications (2)

Publication Number Publication Date
IT8821640A0 true IT8821640A0 (en) 1988-08-04
IT1226367B IT1226367B (en) 1991-01-11

Family

ID=22166288

Family Applications (1)

Application Number Title Priority Date Filing Date
IT8821640A IT1226367B (en) 1987-08-05 1988-08-04 PLANE PILON.

Country Status (8)

Country Link
US (1) US4966338A (en)
JP (1) JPH01101296A (en)
CA (1) CA1316163C (en)
DE (1) DE3826306A1 (en)
FR (1) FR2619076B1 (en)
GB (1) GB2208502B (en)
IT (1) IT1226367B (en)
SE (1) SE504023C2 (en)

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US5779191A (en) * 1996-11-12 1998-07-14 Brislawn; Mark G. Pylon flap for increasing negative pitching moments
GB2359052B (en) * 2000-02-09 2003-09-17 Rolls Royce Plc Engine arrangement
US6685143B1 (en) * 2003-01-03 2004-02-03 Orbital Research Inc. Aircraft and missile forebody flow control device and method of controlling flow
US6964397B2 (en) * 2003-07-18 2005-11-15 The Boeing Company Nacelle chine installation for drag reduction
FR2899200B1 (en) * 2006-03-28 2008-11-07 Airbus France Sas AIRCRAFT WITH REDUCED ENVIRONMENTAL IMPACT
US7770841B2 (en) * 2006-12-22 2010-08-10 Calvin Burgess Inverted airfoil pylon for an aircraft
FR2915179B1 (en) * 2007-04-23 2009-05-29 Airbus France Sa AIRCRAFT WITH REDUCED ENVIRONMENTAL IMPACT.
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US8844265B2 (en) 2007-08-01 2014-09-30 United Technologies Corporation Turbine section of high bypass turbofan
US11149650B2 (en) 2007-08-01 2021-10-19 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US20150377123A1 (en) 2007-08-01 2015-12-31 United Technologies Corporation Turbine section of high bypass turbofan
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11242805B2 (en) 2007-08-01 2022-02-08 Raytheon Technologies Corporation Turbine section of high bypass turbofan
ES2335459B1 (en) * 2007-12-21 2011-02-03 Airbus España S.L. OPTIMIZED CONFIGURATION OF AIRCRAFT ENGINES.
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
US8167237B2 (en) * 2008-03-21 2012-05-01 United Technologies Corporation Mounting system for a gas turbine engine
US8128021B2 (en) * 2008-06-02 2012-03-06 United Technologies Corporation Engine mount system for a turbofan gas turbine engine
US8807477B2 (en) 2008-06-02 2014-08-19 United Technologies Corporation Gas turbine engine compressor arrangement
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8695920B2 (en) 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8511605B2 (en) 2008-06-02 2013-08-20 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8800914B2 (en) 2008-06-02 2014-08-12 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
FR2938504B1 (en) * 2008-11-14 2010-12-10 Snecma AIR INTAKE OF AN AIRCRAFT ENGINE WITH NON-CARINE PROPELLANT PROPELLERS
FR2949754A1 (en) * 2009-09-04 2011-03-11 Snecma Attachment pylon for fixing dual prop jet engine of airplane, has airfoil longitudinally defined between leading edge and trailing edge, and modification unit modifying incidence angle of part of trailing edge
JP5445586B2 (en) * 2009-10-07 2014-03-19 トヨタ自動車株式会社 Wing structure and rectifier
ES2387595B1 (en) * 2009-11-27 2013-08-20 Airbus Operations S.L. METHODS AND SYSTEMS TO MINIMIZE FLOW DISTORSIONS IN THE SHADES OF THE AIRCRAFT OF A AIRCRAFT CAUSED BY FRONT BOLTS
FR2958624B1 (en) 2010-04-08 2012-06-08 Airbus Operations Sas AIRCRAFT TURBOHOMOTING MACHINE, COMPRISING AN INCOMING MOBILE REAR FLAP
US8651426B2 (en) 2010-07-01 2014-02-18 Rolls-Royce Plc Jet engine installation
GB201011056D0 (en) * 2010-07-01 2010-08-18 Rolls Royce Plc Pylon for attaching a gas turbine engine
FR2968634B1 (en) * 2010-12-08 2013-08-02 Snecma PYLONE FOR FIXING AN AIRCRAFT ENGINE WITH NON-CARINE PROPELLANT PROPELLERS
US8622334B2 (en) * 2011-05-19 2014-01-07 Aurora Flight Sciences Corporation System and method for reducing the noise of pusher type aircraft propellers
FR2982236B1 (en) * 2011-11-03 2014-06-27 Snecma HOOK PYLONE FOR TURBOMACHINE
FR2983834B1 (en) * 2011-12-12 2015-01-02 Snecma HOOK PYLONE FOR TURBOMACHINE
WO2015010315A1 (en) 2013-07-26 2015-01-29 Mra Systems, Inc. Aircraft engine pylon
US10371047B2 (en) 2013-10-16 2019-08-06 United Technologies Corporation Geared turbofan engine with targeted modular efficiency
US9533754B2 (en) * 2014-04-19 2017-01-03 The Boeing Company Wing aerial refueling system
US9914528B2 (en) * 2015-02-25 2018-03-13 Embraer S.A. Airframe-integrated propeller-driven propulsion systems
US20170233060A1 (en) * 2016-02-13 2017-08-17 Mra Systems, Inc. Aircraft and empennage section of an aircraft
FR3050721B1 (en) * 2016-04-28 2018-04-13 Airbus Operations AIRCRAFT ENGINE ASSEMBLY COMPRISING A MATTRESS ATTACK EDGE INTEGRATED WITH AN ANNULAR ROW OF OUTER CARRIER OUTPUT GUIDELINES
FR3052743B1 (en) * 2016-06-20 2018-07-06 Airbus Operations AIRCRAFT ASSEMBLY COMPRISING PROPULSION ENGINES BY INGESTION OF THE LIMIT LAYER
US11111029B2 (en) * 2017-07-28 2021-09-07 The Boeing Company System and method for operating a boundary layer ingestion fan
US20190225318A1 (en) * 2018-01-25 2019-07-25 General Electric Company Aircraft systems and methods
US10759545B2 (en) 2018-06-19 2020-09-01 Raytheon Technologies Corporation Hybrid electric aircraft system with distributed propulsion
US10906657B2 (en) * 2018-06-19 2021-02-02 Raytheon Technologies Corporation Aircraft system with distributed propulsion
WO2022198285A1 (en) * 2021-03-24 2022-09-29 Embraer S.A. Longitudinal control surface for aircraft, longitudinal control system for aircraft, and aircraft

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US2142123A (en) * 1938-01-05 1939-01-03 Delmer S Fahrney Extension wing flap
US2257940A (en) * 1938-06-22 1941-10-07 Dornier Werke Gmbh Airplane having a liftable pusher plant
US2406625A (en) * 1941-12-10 1946-08-27 Thomas W Oglesby Airplane
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US3081964A (en) * 1958-12-08 1963-03-19 Boeing Co Airplanes for vertical and/or short take-off and landing
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US3179354A (en) * 1962-04-24 1965-04-20 Alvarez-Calderon Alberto Convertiplane and apparatus thereof
US3191888A (en) * 1963-02-25 1965-06-29 Robert C Sklenka Aircraft having forward and aft propulsion means
US3415468A (en) * 1966-09-19 1968-12-10 Philip D. Labombarde Aircraft
US3572960A (en) * 1969-01-02 1971-03-30 Gen Electric Reduction of sound in gas turbine engines
GB1209723A (en) * 1969-06-14 1970-10-21 Rolls Royce Improvements in or relating to boundary layer air flow
US3599749A (en) * 1969-07-28 1971-08-17 Rohr Corp Jet noise control system
DE2009105A1 (en) * 1970-02-26 1971-09-02 Messerschmitt Boelkow Blohm Noise reduction in propeller engines
US3726091A (en) * 1971-02-16 1973-04-10 Rohr Corp Sound suppressing apparatus
US3695388A (en) * 1971-06-14 1972-10-03 Textron Inc Quiet jet discharge nozzle
US3826331A (en) * 1972-02-29 1974-07-30 Bolt Beranek & Newman Method of and apparatus for reducing sound generated by surfaces in fluid jet streams and the like
US4007896A (en) * 1975-08-08 1977-02-15 Reynolds Iii Collins J Upwardly extendible wing flap system
FR2370171A1 (en) * 1976-11-05 1978-06-02 Snecma METHOD AND DEVICE FOR REDUCING TURBOMACHINE NOISE
GB2107426A (en) * 1981-10-07 1983-04-27 Sidney Walmsley Boundary layer control
US4466587A (en) * 1981-12-21 1984-08-21 General Electric Company Nacelle installation
GB2138507B (en) * 1983-04-22 1987-07-29 Rolls Royce Mounting and exhausting in turbo-propellor aircraft engines
US4685643A (en) * 1983-08-04 1987-08-11 The Boeing Company Nacelle/wing assembly with vortex control device
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Also Published As

Publication number Publication date
GB2208502A (en) 1989-04-05
SE504023C2 (en) 1996-10-21
CA1316163C (en) 1993-04-13
US4966338A (en) 1990-10-30
FR2619076B1 (en) 1994-01-07
GB2208502B (en) 1991-10-02
FR2619076A1 (en) 1989-02-10
SE8802793L (en) 1989-02-06
IT1226367B (en) 1991-01-11
DE3826306A1 (en) 1989-02-16
JPH01101296A (en) 1989-04-19
GB8818581D0 (en) 1988-09-07
SE8802793D0 (en) 1988-08-02

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19950829